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Grade C-6 Titanium vs. C83300 Brass

Grade C-6 titanium belongs to the titanium alloys classification, while C83300 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is grade C-6 titanium and the bottom bar is C83300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290
35
Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 9.0
35
Poisson's Ratio 0.32
0.34
Shear Modulus, GPa 39
42
Tensile Strength: Ultimate (UTS), MPa 890
220
Tensile Strength: Yield (Proof), MPa 830
69

Thermal Properties

Latent Heat of Fusion, J/g 410
200
Maximum Temperature: Mechanical, °C 310
180
Melting Completion (Liquidus), °C 1580
1060
Melting Onset (Solidus), °C 1530
1030
Specific Heat Capacity, J/kg-K 550
380
Thermal Conductivity, W/m-K 7.8
160
Thermal Expansion, µm/m-K 9.8
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.2
32
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
33

Otherwise Unclassified Properties

Base Metal Price, % relative 36
30
Density, g/cm3 4.5
8.8
Embodied Carbon, kg CO2/kg material 30
2.7
Embodied Energy, MJ/kg 480
44
Embodied Water, L/kg 190
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 78
60
Resilience: Unit (Modulus of Resilience), kJ/m3 3300
21
Stiffness to Weight: Axial, points 13
7.0
Stiffness to Weight: Bending, points 35
18
Strength to Weight: Axial, points 55
6.9
Strength to Weight: Bending, points 46
9.2
Thermal Diffusivity, mm2/s 3.2
48
Thermal Shock Resistance, points 63
7.9

Alloy Composition

Aluminum (Al), % 4.0 to 6.0
0
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
92 to 94
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.5
0
Lead (Pb), % 0
1.0 to 2.0
Nickel (Ni), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Tin (Sn), % 2.0 to 3.0
1.0 to 2.0
Titanium (Ti), % 89.7 to 94
0
Zinc (Zn), % 0
2.0 to 6.0
Residuals, % 0
0 to 0.7